Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 27.1015 Oil tank tests
Available versions for ERULES-1963177438-4766
ED Decision 2003/15/RM
found in: CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)
From
CS-27 Amdt 10 - Sm... (Feb 2023)
CS-27 Amdt 9 - Sma... (Dec 2021)
From section
To
CS-27 Amdt 10 - Sm... (Feb 2023)
CS-27 Amdt 9 - Sma... (Dec 2021)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
CS 27.1015 Oil tank tests ED Decision 2003/15/RM Each oil tank must be designed and installed so that it can withstand, without leakage, an internal pressure of 34 kPa (5 psi), except that each pressurised oil tank used with a turbine engine must be designed and installed so that it can withstand, without leakage, an internal pressure of 34 kPa (5 psi), plus the maximum operating pressure of the tank.
CS 27.1015 Oil tank tests ED Decision 2003/15/RM Each oil tank must be designed and installed so that it can withstand, without leakage, an internal pressure of 34 kPa (5 psi), except that each pressurised oil tank used with a turbine engine must be designed and installed so that it can withstand, without leakage, an internal pressure of 34 kPa (5 psi), plus the maximum operating pressure of the tank.